GOE 445 AIRFOIL (goe445-il)
GOE 445 AIRFOIL - Gottingen 445 airfoil
| Details | Dat file | Parser | |
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(goe445-il) GOE 445 AIRFOIL Gottingen 445 airfoil Max thickness 6.4% at 40% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 445 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0070000
0.0250000 0.0105000
0.0500000 0.0155000
0.0750000 0.0190000
0.1000000 0.0220000
0.1500000 0.0265000
0.2000000 0.0290000
0.3000000 0.0315000
0.4000000 0.0320000
0.5000000 0.0295000
0.6000000 0.0255000
0.7000000 0.0210000
0.8000000 0.0150000
0.9000000 0.0083000
0.9500000 0.0045000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0070000
0.0250000 -.0105000
0.0500000 -.0155000
0.0750000 -.0190000
0.1000000 -.0220000
0.1500000 -.0265000
0.2000000 -.0290000
0.3000000 -.0315000
0.4000000 -.0320000
0.5000000 -.0295000
0.6000000 -.0255000
0.7000000 -.0210000
0.8000000 -.0150000
0.9000000 -.0083000
0.9500000 -.0045000
1.0000000 0.0000000
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Polars for GOE 445 AIRFOIL (goe445-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe445-il | 50,000 | 9 | 18.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe445-il | 50,000 | 5 | 19.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe445-il | 100,000 | 9 | 24.2 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe445-il | 100,000 | 5 | 30.8 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe445-il | 200,000 | 9 | 42.4 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe445-il | 200,000 | 5 | 39 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe445-il | 500,000 | 9 | 49.1 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe445-il | 500,000 | 5 | 38 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe445-il | 1,000,000 | 9 | 46.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe445-il | 1,000,000 | 5 | 42.2 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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